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Behavioural Observation of Laminated Polymer Composite under Uniaxial Quasi-Static and Cyclic Loads

机译:层状聚合物复合材料在单轴准静态和循环载荷下的行为观察

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In this study, we investigate the mechanical performance of woven glass fiber reinforced polymer composite laminates subjected to quasi-static and cyclic loading at room temperatures using the unnotched and open hole specimens. The mechanical behaviour and damage in composite laminates are greatly affected by the existence of notches with different parameters such as the size of the holes, number of layers and stacking sequences. The objective of this study is to investigate and evaluate the mechanical behavior of composite lamination structures using unnotched and notched specimens by experimentally and numerically. The materials selected for the studies were chopped strand mat (CSM)/woven roving fabric (WR) as the reinforcement and epoxy resin as the matrix. The hand lay-out technique was used to fabricate these composites. Fractured surfaces were comprehensively examined in a optical microscope and scanning electron microscope (SEM) to determine the microscopic fracture mode and to characterise the microscopic mechanism governing fracture. A numerical procedure based on the finite element method was then applied to evaluate the overall fatigue behaviour of the unnotched and open hole polymer laminate composites using the experimentally applied load. The predicted results based on the FEM analysis were found to be in reasonable agreement with experimental observations.
机译:在这项研究中,我们使用无缺口和裸眼试样研究玻璃纤维增​​强聚合物复合材料层压板在室温下承受准静态和循环载荷的机械性能。复合材料层压板的机械性能和损坏会受到带有不同参数(例如孔的大小,层数和堆叠顺序)的缺口的影响。这项研究的目的是通过实验和数值研究和评估使用无缺口和有缺口试样的复合层压结构的力学性能。选择用于研究的材料是短切毡(CSM)/机织粗纱织物(WR)作为增强材料,环氧树脂是基质。手工布局技术用于制造这些复合材料。在光学显微镜和扫描电子显微镜(SEM)中对断裂的表面进行了全面检查,以确定微观断裂模式并表征控制断裂的微观机制。然后,基于实验施加的载荷,基于有限元方法的数值程序被用于评估无缺口和开孔聚合物层压复合材料的整体疲劳性能。发现基于有限元分析的预测结果与实验观察结果合理吻合。

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